郑州大学学报（工学版）2019，Vol.40Issue(4)：1-7,7.DOI:10.13705/j.issn.1671-6833.2019.04.009
基于遗传算法的变质量航天器姿态控制方法
The Attitude Control Method of Variable Mass Spacecraft Based on Genetic Algorithm
摘要
Abstract
A model independent attitude control method based on genetic algorithm ( GA) was proposed to solve the high-precision attitude control problem of complex and nonlinear uncertain systems such as variable mass characteristic spacecraft. The algorithm optimized the control parameters based on the independent scale of the spacecraft model, without relying on the quality parameter identification of the spacecraft. The simulation results showed that the model independent attitude control method based on genetic algorithm could control the spacecraft with variable mass characteristics under the condition of controlling torque and angular velocity constraints. The algorithm would be of great value for the use of orbiting spacecraft.关键词
变质量特性航天器/遗传算法/在轨服务/姿态控制/模型独立Key words
variable mass characteristic spacecraft/ genetic algorithm/ on-orbit service/ attitude control/model independence分类
航空航天引用本文复制引用
蒋佩华,华冰,黄宇,吴云华,李剑飞,张大伟..基于遗传算法的变质量航天器姿态控制方法[J].郑州大学学报（工学版）,2019,40(4):1-7,7.基金项目
国家自然科学基金资助项目(61673208) （61673208）
